FE Mechanical flashcards
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- Chain rule
- Derivative of a composite function f(g(x)) equals f'(g(x)) times g'(x). Essential for differentiating nested expressions such as sin(x^2) or e^(3x).
- L'Hôpital's rule
- For limits producing 0/0 or ∞/∞, the limit of f/g equals the limit of f'/g' if that limit exists. Apply repeatedly if needed.
- Eigenvalue equation
- For square matrix A, eigenvalues λ satisfy det(A − λI) = 0. Eigenvectors then solve (A − λI)x = 0. Diagonal entries of a triangular matrix are its eigenvalues.
- Dot product
- a·b = |a||b|cosθ = a_x b_x + a_y b_y + a_z b_z. Result is a scalar; zero when vectors are perpendicular. Used for work and projections.
- Cross product
- a×b is a vector perpendicular to both a and b with magnitude |a||b|sinθ. Direction follows right-hand rule. Used for moments and areas.
- Newton-Raphson method
- Iterative root finding: x_{n+1} = x_n − f(x_n)/f'(x_n). Converges quadratically near a simple root but can diverge if the derivative is near zero.
- Binomial distribution
- Probability of k successes in n independent trials with success probability p: P(X=k) = C(n,k) p^k (1−p)^(n−k). Mean np, variance np(1−p).
- Normal standardization
- Convert X ~ N(μ, σ) to standard normal Z = (X − μ)/σ. Then use standard normal tables. Approximately 95% of values lie within μ ± 2σ.
- Central limit theorem
- For large sample size n, the sample mean is approximately normally distributed with mean μ and standard deviation σ/√n, regardless of the population distribution.
- Confidence interval for mean
- With known σ: x̄ ± z_(α/2) σ/√n. With unknown σ and small n: x̄ ± t_(α/2, n−1) s/√n. Width decreases as n increases.
- Coefficient of determination
- R^2 is the proportion of variance in the dependent variable explained by the regression. Ranges 0 to 1; higher values indicate better fit.
- Combinations formula
- Number of ways to choose r items from n without regard to order: nCr = n!/[r!(n−r)!]. For order-sensitive selections use permutations nPr = n!/(n−r)!.
- Paramount public safety
- Under NCEES Model Rules, engineers shall hold paramount the safety, health, and welfare of the public. This duty overrides obligations to employers or clients.
- Responsible charge
- A PE may seal only documents prepared by them or under their direct supervisory control. Sealing work outside responsible charge is a violation of professional conduct rules.
- Conflict of interest disclosure
- Engineers must disclose known or potential conflicts to clients or employers. Accepting compensation from multiple parties for the same service requires full disclosure and consent.
- Qualifications-based selection
- Professional engineering services are typically procured based on qualifications and competence rather than low bid. Price negotiation follows selection of the most qualified firm.
- Negligence elements
- A negligence claim requires duty, breach of duty, causation (actual and proximate), and damages. All four must be shown for liability.
- Effective annual interest rate
- i_eff = (1 + i_nom/m)^m − 1 where m is compounding periods per year. Converts nominal rate to true annual yield; increases with m.
- Capital recovery factor
- (A/P, i, n) = i(1+i)^n / [(1+i)^n − 1]. Converts a present amount to an equivalent uniform annual series over n periods at rate i.
- Internal rate of return
- The interest rate i that makes net present worth equal zero. Accept an independent project if IRR ≥ MARR. Multiple sign changes can yield multiple IRRs.
- Straight-line depreciation
- Annual depreciation D = (B − S)/n where B is first cost, S salvage value, n useful life. Book value after k years = B − kD.
- Breakeven quantity
- Q = FC/(p − v) where FC is fixed cost, p unit price, v variable cost per unit. Produces zero profit; above Q the operation is profitable.
- Resultant of distributed load
- Equivalent force equals the area under the load diagram and acts through the centroid of that area. For uniform load w over length L: R = wL at L/2.
- Zero-force truss member
- A member is zero-force if at a joint with no external load it is the only member in one direction, or if two noncollinear members meet with no load and no support reaction.
- Parallel axis theorem
- I = I_c + A d^2 where I_c is moment of inertia about centroidal axis, A area, d distance between parallel axes. Used for composite areas.
- Beam shear-moment relationship
- dV/dx = −w(x) and dM/dx = V. Bending moment is maximum where shear is zero or changes sign. Area under shear diagram equals change in moment.
- Coefficient of restitution
- e = (v2' − v1')/(v1 − v2) for direct central impact. e = 1 perfectly elastic, e = 0 perfectly plastic (stick together). Momentum is conserved in both.
- Projectile range
- For level ground, range R = v0^2 sin(2θ)/g. Maximum range occurs at θ = 45°. Time of flight t = 2v0 sinθ/g.
- Normal acceleration
- a_n = v^2/ρ = ω^2 r directed toward the center of curvature. Tangential acceleration a_t = dv/dt. Total acceleration magnitude = √(a_t^2 + a_n^2).
- Natural frequency
- Undamped spring-mass system: ω_n = √(k/m) rad/s, f_n = ω_n/(2π) Hz. Damped frequency ω_d = ω_n√(1−ζ^2). Critical damping c_c = 2√(km).
- Torsion formula
- Shear stress in a circular shaft: τ = Tc/J where c is outer radius, J polar moment of inertia. Angle of twist φ = TL/(JG). J = πc^4/2 for solid shaft.
- Flexure formula
- Bending stress σ = My/I where y is distance from neutral axis, I area moment of inertia. Maximum stress at outer fiber: σ_max = Mc/I = M/S.
- Principal stresses
- For plane stress: σ_1,2 = (σ_x+σ_y)/2 ± √[((σ_x−σ_y)/2)^2 + τ_xy^2]. Maximum in-plane shear = √[((σ_x−σ_y)/2)^2 + τ_xy^2].
- Euler buckling load
- P_cr = π^2 EI/(KL)^2 where K depends on end conditions: pinned-pinned 1.0, fixed-fixed 0.5, fixed-pinned 0.7, fixed-free 2.0. Valid for slender columns.